EP0053549A1 - Verfahren zum Befestigen und hermetischen Abdichten eines Stahlgehäuses in der Öffnung eines Aluminiumgehäuses - Google Patents

Verfahren zum Befestigen und hermetischen Abdichten eines Stahlgehäuses in der Öffnung eines Aluminiumgehäuses Download PDF

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Publication number
EP0053549A1
EP0053549A1 EP81401861A EP81401861A EP0053549A1 EP 0053549 A1 EP0053549 A1 EP 0053549A1 EP 81401861 A EP81401861 A EP 81401861A EP 81401861 A EP81401861 A EP 81401861A EP 0053549 A1 EP0053549 A1 EP 0053549A1
Authority
EP
European Patent Office
Prior art keywords
steel
aluminum
housing
strip
enclosure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP81401861A
Other languages
English (en)
French (fr)
Inventor
Colin Anthony Johnson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bendix Corp
Original Assignee
Bendix Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bendix Corp filed Critical Bendix Corp
Publication of EP0053549A1 publication Critical patent/EP0053549A1/de
Withdrawn legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
    • B23K31/02—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to soldering or welding
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/46—Bases; Cases
    • H01R13/52—Dustproof, splashproof, drip-proof, waterproof, or flameproof cases
    • H01R13/5202—Sealing means between parts of housing or between housing part and a wall, e.g. sealing rings
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/46—Bases; Cases
    • H01R13/516—Means for holding or embracing insulating body, e.g. casing, hoods

Definitions

  • This invention relates to hermetically sealing together steel and aluminum and is more specifically related to hermetically sealing a steel connector housing to the opening in an aluminum housing for a jet engine exciter.
  • connection between the steel connector with an aluminum enclosure is usually made by soldering with a solder having a tin and lead content of about 60/40.
  • solder having a tin and lead content of about 60/40.
  • such an alloy looses much of its strength at elevated temperatures and is, therefore, not normally used at temperatures over 250 degrees Fahrenheit. Consequently, aluminum housings with steel connectors, although lighter, have temperature limitations and usually mechanically weak soldered joints.
  • the present invention proposes a method of attaching and hermetically sealing a steel housing to the opening in an aluminum housing, characterized in that it comprises the steps of:
  • This invention provides a method of fusion welding a steel connector housing to an aluminum exciter enclosure to provide a hermetic seal between the two.
  • the invention is characterized by the use of a roll bonded strip of steel and aluminum arranged between the connector housing and enclosure opening so that the steel portion of the strip faces and contacts steel and the aluminum portion of the strip faces and contacts aluminum.
  • the exposed demarcation lines or seams between the same materials i.e., steel and steel, are fusion welded to provide a hermetic seal.
  • Another advantage of this invention is that it provides a jet engine exciter assembly that is lighter in weight and can be exposed to higher temperatures and altitudes without loss os hermeticity.
  • Another advantage of this invention is that it provides a stronger connection between a connector housing and an exciter enclosure made of dissimilar metals.
  • Another advantage of this invention is that it provides a less expensive and faster means of connecting a steel connector housing to an aluminum jet engine exciter enclosure.
  • Another advantage of this invention is that it eliminates soldering of connections between steel connector housings and aluminum jet engine exciter enclosures so as to eliminate the use of expensive filler metals and electroplating necessary'with soldering techniques.
  • FIG. 1 illustrates a jet engine exciter enclosure 1 having attached thereto one or more electrical connectors 20.
  • Each electrical connector 20 includes a flange or shoulder 21 that may be comprised of steel or aluminum. If comprised of steel, it is connected to an aluminum enclosure 1 by a washer shaped roll bonded strip of aluminum and steel arranged so that the aluminum portion 32 of the strip faces and contacts the aluminum portion 32 of the strip faces and contacts the aluminum enclosure.1 and the steel portion 31 of the roll bonded strip faces and contacts the steel shoulder 21 of the connector 20. Since the aluminum and steel is roll bonded together, there is a hermetic seal between the two materials of the strip where they interface.
  • Figures 2 Illustrates an end view of the jet engine exciter assembly shown in Figure 1 and illustrates how the second fusion weld 34 extends along the entire junction or seam between the aluminum portion 32 of the strip and the aluminum exciter housing 1 and the first fusion weld 33 extends along the entire junction between the steel portion of the strip and the steel connector housing 20. Fusion welds 33 and 34 completely seal the enclosure 1.
  • Figure 3 Illustrates a connector assembly 40 which does not have an annular shoulder on the outside thereof. Accordingly, a ring shaped roll bonded strip 30 of aluminum and .steel is placed in the space between the connector housing 40 and the enclosure1. In this arrangement, the fusion welds 33 and 34 also extend completely around the seam between the aluminum portion 32 of the strip 30 and the enclosure 1 and the seam between the steel portion 31 of-the strip 30 and the conncector housing 40.
  • Figure 4 is another arrangement of a jet engine exciter enclosure 1 where the opening includes a protrusion
  • fusion welds 33 and 34 extend 360 degrees around the connector 40 to completely and hermetically seal the inside of the enclosure 1 from the outside air.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Casings For Electric Apparatus (AREA)
  • Gasket Seals (AREA)
EP81401861A 1980-11-28 1981-11-24 Verfahren zum Befestigen und hermetischen Abdichten eines Stahlgehäuses in der Öffnung eines Aluminiumgehäuses Withdrawn EP0053549A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US21094580A 1980-11-28 1980-11-28
US210945 1988-06-23

Publications (1)

Publication Number Publication Date
EP0053549A1 true EP0053549A1 (de) 1982-06-09

Family

ID=22784974

Family Applications (1)

Application Number Title Priority Date Filing Date
EP81401861A Withdrawn EP0053549A1 (de) 1980-11-28 1981-11-24 Verfahren zum Befestigen und hermetischen Abdichten eines Stahlgehäuses in der Öffnung eines Aluminiumgehäuses

Country Status (2)

Country Link
EP (1) EP0053549A1 (de)
JP (1) JPS57118890A (de)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3495319A (en) * 1966-10-25 1970-02-17 Kaiser Aluminium Chem Corp Steel-to-aluminum transition joint

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2177284A5 (de) * 1972-03-23 1973-11-02 Burroughs Corp

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3495319A (en) * 1966-10-25 1970-02-17 Kaiser Aluminium Chem Corp Steel-to-aluminum transition joint

Also Published As

Publication number Publication date
JPS57118890A (en) 1982-07-23

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Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19811126

AK Designated contracting states

Designated state(s): DE FR GB IT

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19830321

RIN1 Information on inventor provided before grant (corrected)

Inventor name: JOHNSON, COLIN ANTHONY